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Published in 2017 at "Experiments in Fluids"
DOI: 10.1007/s00348-017-2310-5
Abstract: This study describes the application of a novel damping insert material for reducing the flow fluctuations in a tandem nozzle supersonic wind tunnel. This new damping material is composed of multi-layer stainless steel wired meshes.…
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Keywords:
test section;
multi layer;
supersonic wind;
damping insert ... See more keywords